Pressure Bifurcation Phenomenon on Supersonic Blowing Trailing Edges-Reference-Cited by-同舟云学术

Pressure Bifurcation Phenomenon on Supersonic Blowing Trailing Edges

Published:2019-01 Issue:1 Volume:57 Page:153-164
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Martinez-Cava Alejandro¹,Wang Yinzhu¹,Vicente Javier de¹,Valero Eusebio¹

Affiliation:

1. Technical University of Madrid, E-28040 Madrid, Spain

Funder

H2020 Marie Skłodowska-Curie Actions

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057056

Reference44 articles.

1. NashJ. F. “A Review of Research on Two-Dimensional Base Flow,” Aeronautical Research Council R&M No. 3323, Great Britain, 1963, pp. 1–25.

2. NashJ. F. “A Discussion of Two-Dimensional Turbulent Base Flows,” Aeronautical Research Council R&M No. 3468, Great Britain, 1967, pp. 1–46.

3. NashJ. F.QuinceyV. G.CallinanJ. “Experiments on Two-Dimensional Base Flow at Subsonic and Transonic Speeds,” Aeronautical Research Council R&M No. 3427, Great Britain, 1966, pp. 1–34.

4. Experimental studies on the lip shock.

5. The Base Pressure Problem in Transonic Turbine Cascades

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of thermal performance in dual‐fuel units;Energy Science & Engineering;2022-09-28

2. Efficiency of Pulsating Base Bleeding to Control Trailing Edge Flow Configurations;Applied Sciences;2022-07-04

3. Stochastic boundary condition effects on supersonic leading edge blowing;Computers & Fluids;2022-07

4. Characterization of base bleed effects on subsonic trailing edge flows;Aerospace Science and Technology;2021-06

5. Oscillations of transonic flow past a symmetric profile with a blunt trailing edge;Vibroengineering PROCEDIA;2021-05-07